Electrochemical and hot corrosion behaviour of steel reinforced with AlSiBeTiV high entropy alloy using friction stir processing

ABSTRACT A lightweight AlSiBeTiV high entropy alloy (HEA) powder is synthesized by the ball milling process and is reinforced on SS410 through friction stir processing (FSP). Subsequently, the annealing process is conducted on the processed samples at 450, 600, and 750°C for 120 mins. The grains are refined at 600°C by 23.3% than the processed HEA sample. A higher microhardness of 672 HV is attained on the processed HEA sample annealed at 600°C due to the synergistic effect of FSP and annealing through refined grains. The electrochemical corrosion under a 3.5 wt.% NaCl environment, and the hot corrosion under the salt mixture environments of 75% Na2SO4 +25% NaCl, and 60% Na2SO4 +20% NaCl + 20% V2O5 at 800°C for 50 h are investigated on the processed samples. The microstructure, induced corrosion products, and elemental distribution of the corroded surface of the annealed processed HEA sample are evaluated by morphological analysis. The induced oxidation effect enhances the Cr2O3 and TiO2 films on the corroded surfaces leading to higher corrosion resistance. A high corrosion resistance appears on the annealed processed HEA sample through the formation of a stable passive layer, hindering the pitting corrosion mechanism, grain refinement, and homogeneous distribution.


Introduction
Steels are widely used in engineering industries since the nineteenth century due to their durability in various environments.The different categories of steel are available for many applications such as aerospace, automotive, military, construction, transport, oil, and gas industries.The properties of steel include high fracture toughness, impact strength, formability, weldability, and corrosion resistance even at elevated temperatures.The material properties are degraded over the duration due to corrosion and erosion under fluid environments such as marine applications, chemical, and nuclear industries.The stainless steels are most applicable for corrosion nature [1,2].Numerous processing methods are customized to extend the application of materials in engineering and medical sectors.It encompasses surface coating, annealing, microstructural modifications, additive manufacturing, and so on.Additional fine layers are added around the surface of the samples by coating.These layers are developed by cladding, sputtering, vapour deposition, and thermal spray techniques.The reinforced materials are delaminated due to machining and the corrosion environments for a long period.The surface distortion by materials degradation leads to micro-cracks and phase structure deformation [3].A surface modification technique is used to overcome the above issues and withstand erratic environmental conditions.One of the single-step and ecofriendly processing techniques is employed to enhance the properties of materials for ensuring their applications.Such a process is termed friction stir processing (FSP) which is obtained from friction stir welding.FSP is one of the green techniques to achieve improved properties by microstructural modification [4].The grain refinements in the processed zone lead to high mechanical properties, corrosion, and wear resistance through various strengthening mechanisms [5,6].The microstructural modification of SS316L by FSP leads to increased microhardness, tensile, and yield strength by 24.7%, 29%, and 18% respectively to the base sample.The refined grains by dynamic recrystallization (DRX) and exclusion of pores in the processed zone are attributes to the enhanced strengthening mechanism [7].The FSP employed on AISI 440C stainless steel reveals a high hardness of 779 HV through refined grains on the stir zone (SZ) by localized plastic deformation.The increased Cr elements by the dislocation of carbides lead to increased pitting resistance on the processed zone [8].A 2507 duplex steel is processed by FSP to improve mechanical properties.The processed sample exhibits a higher microhardness of 392 HV, tensile strength of 937 MPa, and yield strength of 755 MPa over the base sample.The FSP processed sample improves corrosion resistance than the base sample under the 3.5 wt.% NaCl environment.The amended stability and passivation film are generated on the processed sample due to the refined grains that lead to higher corrosion resistance [9].The refinement of grains is the major feature of FSP for enhancing material properties.Subsequently, FSP (Lakshmi Machine Works Limited, Coimbatore, India) is used to reinforce the filler material with the base sample for further improvement in the results.
FSP is used to reinforce nano-SiO 2 powder to AZ91 magnesium alloy and microstructure characterization is revealed under various process parameters.An increased traverse speed of the FSP leads to 1.9 and 2.1 times higher hardness and tensile strength in the SZ through refined grains than the base sample.The DRX and induced frictional heat by the maximum traverse speed cause a refined grain structure [10].Al 2 O 3 and carbon nanotubes are reinforced on AA6061 alloy by FSP.The reinforced and processed samples exhibit increased microhardness, ultimate tensile strength (UTS), and yield strength by 63.7%, 22.3%, and 73.6%, respectively, than the processed base sample.The grain reduction, Hall-Petch relationship, and Zener pinning effect are attributes to the improved strengthening results.The excellent interfacial bonding of reinforced particles on the dimple of fractured samples also leads to improved tensile and yield strength [11].The SS316 steel powder is reinforced on AA6061 alloys through H13 tool steel by FSP.The processed samples exhibit an increased hardness of 139 HV and tensile strength of 279.9 MPa through refined grain size by higher tool rotational speed.The severe plastic deformation (SPD) and DRX lead to high corrosion and wear resistance.The refined grain size, evenly distributed filler materials over the base sample, maintaining the strengthening phase of Mg 2 Si, and flow of reinforced material are attributes to the enhanced properties [12].The additional improvement of processed samples through microstructural modification and reduction of internal stress is achieved by a subsequent process.Such a process is termed a heat treatment, utilized for the recrystallization of grain structures.Many heat-treatment processes are available to improve the mechanical properties of materials.Annealing is one of the processes that improve the properties of steel effectively by recovery, recrystallization, grain growth, and homogenization [13] The FSP is used to reinforce SiC material on the Ti-6Al-4 V composite.The processed samples further undergo heat treatment for additional improvement of mechanical properties.The superior interfacial bonding of SiC with the base sample causes higher mechanical properties and wear resistance.The heat-treated processed sample exhibits deep and fine dimples on the fractured surface leading to ductile fracture.The shallow grooves without wear debris appeared on the worn surface of heat-treated samples [14].
A new class of material is derived very recently to meet the current challenges in engineering industries.The designed material is composed of five or more elements with a 5-35% atomic percentile, labeled as high entropy alloy (HEA).The synthesized HEA particles have higher mechanical properties even at elevated temperatures due to their owning characteristics.It includes high specific modulus, excellent strength with ductility, high hardness, and fatigue strength [15][16][17].The formation of a singlephase solid solution is one of the crucial processes, and it could be obtained by high entropy with low Gibbs free energy [18].The CoCrFeMnNi HEA particles are synthesized by gas atomization followed by the hotpressing sintering process at 1100°C.The equiatomic HEA particles exhibit a homogeneous distribution of face-centered cubic (fcc) structure with an average grain size of 16 μm.A higher yield strength of 358 MPa and UTS of 778 MPa are obtained by nanosized metastable structured HEA particles.The synergetic effect of grain refinement and nano-sized crystal structures causes a strengthening mechanism in fabricated HEA particles [19].The mechanical alloying employed to synthesize MoNbTaTiV HEA powder yields a body-centered cubic (bcc) phase structure.The HEA particles with a mean size of 15 nm are obtained by the dissolution and diffusion of multicomponent elements after the 40 h milling.The homogeneous distribution of HEA powder appears by refined grains and high lattice strain.The nano-sized particles sustain the bcc phase at 800°C to 1200°C which is evidence of high thermal stability [20].
Thus, the extensive literature studies reveal limited work is conducted on steel by reinforcing HEA particles to enhance the mechanical and corrosion properties.A first attempt is made on reinforcing lightweight AlSiBeTiV HEA particles over the SS410 base sample by FSP followed by annealing at different temperatures to analyze the microstructure and corrosion behaviours.The corrosion behaviour of processed samples is investigated through electrochemical corrosion and hot corrosion under different salt mixture environments.The microstructural characterization, microhardness, and corrosion behaviours of the processed HEA sample after annealing are evaluated and the results are compared with the processed HEA sample before annealing to study the effect of annealing.The morphological analysis of corroded samples evaluates the corrosion products, and induced oxide layers with corrosion mechanism.

Materials preparation
The HEA is a design-based alloy and consists of quinary elements such as Al, Be, Si, Ti, and V.The chemical composition of HEA powder is tabulated in Table 1.To enhance the corrosion resistance, Ti and V are contributed as the principal elements.These elements produce a high corrosion resistance by forming a passive film that is stable even at high temperatures [21].To achieve high strength and ductile properties with less density, Al is added as one of the multifunctional elements [22].Greater oxidation resistance is exhibited by the addition of Al and Si through the formation of a protective oxide layer [23].The grain refinements improve by the addition of lowdensity Be element [24].Hence, the developed powder produces superior strength, mechanical properties, and higher corrosion resistance.The selected individual powders are ball-milled with equiatomic percentile at a speed of 250 rpm for 20 h.To prevent the cold welding of HEA powders during the process, 5 wt.% stearic acid is added as a process control agent.The ball-to-powder ratio of 10:1 with a tungsten carbide milling vial is used for a significant milling process.The fabricated HEA powders are reinforced over the base sample by FSP.In the present work, the Stainless Steel of grade 410 (SS410) is chosen as the base sample due to the presence of the Cr element with 12.8%ile and excellent corrosion behaviour at elevated temperatures.Figure 1 demonstrates the sequence of the present research work.SS410 finds numerous applications related to corrosion environments.It includes storage tanks in chemical and nuclear industries, gas turbines, and petroleum fractionating structures [25].The SS410 steel is acquired from the commercial industry and sized by wire cut-electrical discharge machining (EDM).The elements present in SS410 are tabulated in Table 2.

Friction stir processing
The microstructural modification by refined grains is one of the prime functions of FSP.The rotational speed, traverse speed, and applied load are the controllable parameters of FSP, which are attributed to the frictional heat and SPD.The synergetic effect of the downward applied load and rotary action of the FSP tool generates sufficient heat by the frictional action.A trapezoidal slot is machined on a 100 × 100x6 mm 3 base sample with a dimension of 2 mm, 4 mm on the base, and 4 mm depth machined by wire cut-EDM at the center of the surface.A pinless tool is employed to compact the HEA powder in the machined slot.A WC tool of 16 mm diameter cylindrical profile and tapered pin (2:3) of 4.5 mm length is used to reinforce HEA powder over the base sample.The FSP is accomplished with process parameters of 950 rpm tool rotation and 20 mm/min traverse speed with a 10 kN downward applied force.The combined effect of higher rotational speed and lower transverse speed is attributed to refined grains in the SZ [4] The optimized process parameters lead to an equalized grain reduction in the SZ by homogeneous nature.To investigate the annealing effect, the processed samples are subjected to 450°C, 600°C, and 750°C for 120 mins.The properties of processed samples after annealing are compared with the processed samples before annealing to study the effect of annealing on corrosion behaviour.The processed base sample and processed HEA sample before annealing are represented by P Base , P HEA and after annealing are represented by A Base , A HEA respectively.Figure 2 shows the SZ, thermomechanically affected zone (TMZ), heat-affected zone (HAZ), and base material (BM) of the processed sample.

Materials characterization
The microstructural analysis of ball-milled HEA powder is carried out by scanning electron microscopy (SEM) analysis.The elemental mapping and distribution of multicomponent elements in the HEA particles are evaluated by energy dispersive X-ray spectroscopy (EDS).The SEM and EDS analyses are conducted with ZEISS Gemini SEM 300 equipment at an acceleration voltage of 10 kV.The phase structure of HEA powder is analyzed by X-Ray diffraction (XRD) using Empyrean setup from Malvern Panalytical.The AlSiBeTiV HEA powder is directed and placed in the specimen holder for the materials characterization.
The microstructural characterization of the processed samples is conducted with the same specification.
A 10 × 10x6 mm 3 volume is sized by wire cut-EDM in the SZ of the processed samples for morphological evaluation.The surface of the samples is polished with different grit sizes of emery sheets for characterization.
The ASTM E11 standard is followed for the microstructural evaluation.The SEM, EDS, and XRD evaluations are made on processed samples for their microstructural characterization.The electron backscatter diffraction (EBSD) is performed on the A HEA to evaluate the refined grains and their distribution in the SZ.The microhardness of processed samples is conducted by a Mitutoyo-made Vickers hardness tester according to ASTM 384.The hardness test is performed on the SZ with a diamond indenter and applied load of 100 g for 15 s dwell period.The rhombus-shaped indentation on the surface of the sample is measured by micrometre scales which are integrated with the equipment.

Corrosion behaviour
The corrosion behaviour of processed samples at room temperature is analyzed by an electrochemical corrosion test.The wire cut-EDM is employed to size the samples by 15 × 15x6 mm 3 according to ASTM G59 for corrosion behaviour.The prepared samples are placed under the 3.5 wt.% NaCl environment on electrochemical corrosion tester Versastat 3-400 equipment for electrochemical corrosion.The corrosion behaviour of processed samples is exhibited in the form of a potentiodynamic polarization (PDP) plot.The electrochemical test is performed with three electrode flat cells.The saturated calomel and platinum electrodes are considered as reference and counter electrodes respectively.In addition, the prepared test sample served as the working electrode.The polarization range, rate, and frequency are set at − 0.5 to 0.5 V, 1 mV/s, and 0.5 Hz respectively for 30 mins.The hot corrosion behaviour of processed samples is evaluated under the two different salt mixtures at 800°C for five cycles in 10 h intervals.The salt mixtures are prepared by the high-purity mixture of Na 2 SO 4 , NaCl, and V 2 O 5 salts dissolved with distilled water.A 3:1 ratio of Na 2 SO 4 and NaCl mixed salts is termed salt mixture A and a 3:1:1 ratio of Na 2 SO 4 , NaCl, and V 2 O 5 mixed salts is termed salt mixture B. Initially, the processed samples are heated up to 130°C for removing moisture content, and the initial weight is measured by an electronic weighing machine.
The prepared salt mixtures are applied on the surface of the samples as a thin film until uniform distribution is attained.Then, the salt mixture film applied samples are kept in the resistance furnace at 800°C for 50 h.The weight of the corroded samples is measured at 10 h intervals during the experimentation.The morphological studies are performed on the corroded surface of the A HEA to evaluate corrosion products and compare them to the P HEA .

Microstructural characterization of HEA powder
The characterization of synthesized AlSiBeTiV HEA powder is analyzed by SEM evaluation.The ballmilled HEA particles are densely packed with irregular fragments as shown in the SEM image (Figure 3a).The equisized HEA particles are homogeneously distributed.The particles with an average size of 15 µm are obtained in the fabricated HEA powder.A singlephase fcc structure with the absence of intermetallic peaks appears in the HEA powder as shown in Figure 3b.The existence of elements in HEA particles with their atomic percentile is evaluated by EDS analysis (Figure 3c).A fewer number of foreign substances appear in the powder from the ball during the milling and the effect of these elements is negligible.The present elements are close to equal to that confirmed by the EDS mapping.

Microstructural characterization of P HEA
Microstructural characterization of the P HEA is evaluated by morphological investigation.The defectfree surface is obtained by FSP through sufficient induced frictional heat.The SEM image shows the refined grain structure in the SZ (Figure 4a).The grains of the P HEA exhibit more refinements in the SZ as compared to the thermomechanical and heataffected zones.The equiaxed grains are evenly distributed in the SZ of the P HEA .Refined grains are generated in the SZ by DRX.During the FSP, grain size reduction and grain growth occur simultaneously over the SZ due to the dynamic recrystallization.The grain size increases by induced frictional heat on FSP.The generation of nucleation effects by the stirring action of the FSP tool leads to refined grains in the SZ [26].Besides, the grain growth is controlled by reducing dislocation movements by the hindering effect of the HEA particles.The discontinuous DRX is attributed to refined grains along with sub-grain boundaries [27].DRX and SPD are the routes of grain refinement, which is the major role of FSP.The cross-sectional view of the processed HEA sample exhibits a better interfacial bonding between HEA particles and the base sample (Figure 4b).During the deformation, the interfacial bonding causes a hindering effect on dislocation movements and leads to enhanced properties.The EDS evaluation is performed to verify the elements and their percentile on the P HEA (Figure 4c).XRD evaluates the phase structure of the P HEA and reveals to be a singlephase fcc structure with the absence of any intermetallic peaks as depicted in Figure 4d.Moreover, the P HEA holds up the same phase structure of HEA powder attributed to higher thermomechanical stability.The line mapping evaluation performed on the P HEA crosssectional surface is shown in Figure 5a.The elements present in the HEA particles and their percentile across the mapped line in the cross-section of the P HEA are affirmed by the EDS mapping plot (Figure 5b).

Microstructural characterization of A HEA
The annealed processed samples exhibit recovery, recrystallization, and grain growth by the given temperatures.The morphological evaluation of the A Base and A HEA under three annealing temperatures are shown in Figure 6.There are no obvious differences between A Base and A HEA at 450°C (Figure 6a,d).The microcracks are minimized in some of the regions due to stress released at 450°C.The softening and ductile properties are improved in the samples at 450°C.The annealed samples exhibit unequalised grains demonstrating the absence of a recrystallization process and elongation of grains observed.More refined grains are observed in both the A Base and A HEA for the increment of annealing temperature to 600°C (Figure 6b,e).The refined uniform grains are formed in the SZ which enhances the mechanical properties of annealed samples.The A HEA exhibits homogeneous refined grains at 600°C and is free from the microcracks.The equalized refined grains with uniform distribution and a higher degree of recrystallization enhance the material properties in the A HEA .The refined grains with uniform size structure confirm the recovery and recrystallization of samples at 600°C.Subsequently, the refined grains are increased in size with the addition of the annealing temperature up to 750°C (Figure 6c,f).The fine grains are replaced by the formation of coarse grains with reduced dislocation density and smooth grain boundaries [28].Hence, the sample after annealing at 750°C leads to a decline in strengthening properties by the increment of plasticity at the elevated temperature [29].The high solid solution phase is obtained by lower Gibbs free energy of HEA and impediments of intermetallic growth are caused by the effect of the annealing process.The evenly distributed grains with uniform size and high- entropy effects lead to high corrosion resistance.The corrosion resistance is enhanced by dissolving the segregation phase at the elevated temperature that induces the homogenization of grains [30].
The elemental mapping and presence of element distribution in the SZ of the A HEA at 600°C is shown in Figure 7a.The HEA elements are evenly distributed on the SZ of the A HEA to improve the properties.The EDS plot express the presence of HEA elements with their percentile in the SZ (Figure 7b).The reinforcing HEA particles are entrenched on the SZ with no cluster.A better metallurgical bonding on the interface of the reinforced HEA particle with the base sample is evidenced by EDS mapping.The refined grains by annealing at 600°C led to improve interfacial bonding effectively.The line mapping on the A HEA at 600°C is shown in Figure 8a.The HEA elements and their distribution across the mapped line along with their percentile are confirmed by EDS evaluation (Figures 8b,c).The fcc phase structure with the absence of intermetallic phases is identified by the XRD pattern (Figure 8d).The annealing process also confirms the same phase which is obtained on the HEA powder and P HEA which implies a higher thermomechanical ability after annealing at 600°C.

EBSD analysis of A HEA
The FSP and annealing process plays a major role to enhance the strengthening properties of A HEA by grain refinement.EBSD analysis is used to evaluate the refined grain size with their distribution in the SZ of the A HEA (Figure 9a).The inverse pole figure (IPF) shows more distinct grains in the crystallographic direction than the rolling direction.The DRX and SPD lead to refined grains in the SZ of the A HEA due to the annealing and FSP [31].The synergetic effect of annealing after FSP attributes to more refined grains in the SZ of the A HEA .The evenly distributed grains in the size of 0.138 µm to 3.31 µm appear on the A HEA (Figure 9b).An average grain size of 0.527 µm is obtained on the SZ by the influence of annealing, which is reduced by 23.3% than the P HEA [32].A 51% of high-angle grain boundaries (HAGB >15° misorientation angle) obtained in the SZ is indicated by the blue line on boundary mapping which is due to the DRX and continuous dislocation (Figure 9c).A 49% of low-angle grain boundaries (LAGB −2° to 15° misorientation angle) obtained in the SZ is indicated by the red line on boundary mapping which is due to the dislocation movement and induced subgrain boundaries.The analysis reveals a high fraction   of HAGB obtained than the LAGB (Figure 9d).The evenly distributed grains by the effect of FSP through DRX and SPD are refined by the annealing process [33].The deformation energy storage of the processed sample by FSP, the relationship of lattice distortion and micro-strain in a crystalline structure are described by kernel average misorientation (KAM) map as shown in Figure 9e.The high deformation energy storage exhibited in the A HEA that enhances the DRX and impediment of grain size [31].Figure 9f shows the refined grains in red which is evidence of < 111> texture formation in the A HEA .The high Schmid factor in the SZ is by the homogeneously distributed nanograins with uniform size and it improves corrosion resistance and strength [34].

Evaluation of microhardness
To measure the significance of the annealing, the microhardness of the annealed samples are compared with unannealed samples as shown in Figure 10.The A HEA at 600°C exhibits 672 HV microhardness which is 29.7% higher than the P HEA .Moreover, the P HEA demonstrates 518 HV microhardness which is higher than the A Base showcasing the enhancement of reinforced HEA particles.The grain refinement through DRX and SPD by FSP and subsequent annealing are the foremost features for enhanced microhardness.The microhardness of A HEA and A Base is increased linearly with the increase in annealing temperature at a certain range.An optimum microhardness is obtained on the A HEA at 600°C.The further increase of temperature declines the microhardness of the A HEA at 750°C.The grain growth at higher annealing temperature decreased the microhardness [28].The homogeneous distribution of HEA particles and the formation of HAGB in the SZ of the processed sample leads to higher hardness [35,36].The reinforced HEA particles hinder the dislocation movement during deformation attributed to enhanced hardness.The equiaxed refined grains, quench hardening effect improves the hardness [37,38].Moreover, the lattice distortion, sluggish diffusion effects of reinforced HEA and exceptional strengthening mechanism by FSP attribute significant grain refinements which lead to higher microhardness [39].Initially, the recovery stage of annealing diminishes microhardness due to the surface softening.The reduced microhardness is reimbursed and improved during the recrystallization stage of annealing through fine grains and stress reliving which is developed during the FSP process [40].The synergistic effect of DRX and SPD of FSP is attributed to superior grain refinement that improves the microhardness according to the report of the Hall-Petch relationship [26,41,42].Besides, the bonding features of reinforced HEA particles with base metal also lead to enhanced microhardness.

Electrochemical corrosion behaviour
The effect of annealing on the corrosion behaviour of the processed samples is analyzed under the 3.5 wt.% NaCl solution by a PDP curve.The electrochemical corrosion mechanism under a salt environment is illustrated in Figure 11.It shows the formation mechanism of the corrosion products and oxide layer along with cracks and delaminated surfaces.The PDP curve of corroded samples is shown in Figure 12a.The corrosion potential (E Corr ), current density (I Corr ), and tafel constants (β a & β b ) of corroded samples are obtained from the PDP curve and are tabulated in Table 3.The E Corr value of the A HEA is more positive than the P HEA , A Base , and P Base .Subsequently, the A HEA exhibits a low value of I Corr as compared to the P HEA , A Base , and P Base .The E Corr represents the reactivity of materials and a higher value of E Corr leads to more stability under the corrosion environment.However, the corrosion rate is indicated by I Corr and low values of I Corr represent higher corrosion resistance [30].The reinforced HEA particles exhibit a high entropy effect attributing to the enhancement of the passive layer for hindering corrosion of the underlying base sample.The corrosion resistance of the A HEA is improved by impeding the formation of local anodic sites through the presence of quinary elements of HEA particles [43].The reinforcement of HEA particles with the base sample leads to reducing the corrosion effect by developing a passive layer [44].The characteristics of the oxide layer are significantly influenced by the donor-to-acceptor ratio of the passive layer.Normally, a decreased donor-to-acceptor density is exhibited in the refined grain structure.The improved   passivity is obtained by the reduction of available charge carriers and reduces donor-to-acceptor ratio in the corrosion environment.The ratio is decreased continuously in the chloride environment and the Cl ions tend to relocate vacancies of oxygen in the passive film.Hence, the earlier passivation kinetics appeared through refined grain structure by FSP exhibits a stable and predominant resistance to corrosion nature [45].The grain size of samples also plays a predominant role in the corrosion behaviour [46].The excellent passive layer obtained in the A HEA leads to improved corrosion resistance than the P HEA through refined grains by the annealing process.The A HEA exhibits strong passivation by the HEA particle diffusion during the grain refinement through FSP and annealing.The polarization resistance (Rp) of the corroded samples is calculated by the Stern-Geary Equation (1).A higher value of Rp indicates improved corrosion resistance.Besides, the inverse relationship is exhibited on I corr with Rp as per the Stern-Geary equation.Generally, the increasing rate of cathodic and anodic reactions directly infers to the increment in I corr value, thereby a decrement in polarization resistance.The generation of a passive layer on the corroded sample surfaces aids with improved corrosion resistance [47].
The reinforced AlSiBeTiV HEA particles lead to hindering crack propagation thereby improving corrosion resistance.The homogeneously distributed HEA particles over the base sample and metallurgical bonding of HEA particles with the base sample through FSP also contribute to higher corrosion resistance [48].The higher value of E Corr , diffusion of HEA elements, and fine grains of the A HEA support the formation of a thin and stable passive layer that enhances corrosion resistance.The Nyquist plots of the corroded samples are shown in Figure 12b.The higher capacitive loop infers improved corrosion resistance.The capacitive loop of P Base and A Base is measured to be 2500 Ω cm 2 and 3750 Ω cm 2 in diameter.However, the P HEA and A HEA is measured to be 4500 Ω cm 2 and 5500 Ω cm 2 in diameter.The higher value of the capacitive loop in diameter indicates a higher potential that enhances corrosion resistance [49].Hence, the A HEA shows an improved corrosion resistance in the PDP curve and Nyquist plots.The corrosion rate of processed samples is calculated from the electrochemical corrosion parameters by using Faraday's Law.

Corrosion rate ¼ K 1 I corr EW ρ
where, K 1 is a constant and the value of 3.27 × 10 −3 mm/ μAcmyear, corrosion current density (I corr ) in μA/cm 2 , equivalent weight (EW) in g/equivalent, and density (ρ) in g/cm 3 .Figure 13 shows the corrosion rate of processed samples under the 3.5 wt.% NaCl environment.A higher corrosion rate is obtained on the P Base than the other samples.The P Base is more easily corroded under the NaCl environment than the A Base .Pitting corrosion is the predominant factor of the P Base for a higher corrosion rate.The A HEA exhibits a low corrosion rate against other samples.The reinforced HEA particles lead to optimal corrosion rate by high stability of its constituent elements.However, the A HEA surface reduces the corrosion rate than the P HEA by improved grain refinements, homogeneous microstructure, and a stable passive layer around the corroded surfaces due to the annealing.The morphological evaluation of corroded samples under the NaCl environment is analyzed by SEM (Figure 14).The P Base is severely corroded under the NaCl environment as compared to the A Base (Figure 14a).Some regions of the P Base surfaces exhibit stable pits and micropores expanded to large-sized holes.The inadequate adherent metal chlorides and oxides are formed along with porous on the surfaces of the base sample due to the reaction of chloride ions with the steel surface [50].The corrosion pits are randomly dispersed on the P Base surface and pitting corrosion is a dominant factor.The dark region on the corroded surface is observed to be localized pitting corrosion.A few regions of the A Base surface exhibit pitting corrosion with cracks and is reduced by the refined grains through annealing (Figure 14b).The unstable hemispherical pits are formed on the A Base surface.The open cavity in the form of hemispherical nature is exhibited on the corroded surface due to the collapsed thin layer of pits.The formed pit layer is very thin, in the order of a few micrometers.The covered layers are perforated by further undercutting events and it leads to material dissolution [51].The pitting corrosion mechanism reduces the corrosion resistance [52].A stable oxide layer in the form of Cr 2 O 3 and TiO 2 with few cracks and pitting corrosions is observed on the P HEA surface (Figure 14c).The oxide layers of Cr 2 O 3 and TiO 2 are confirmed by the XRD pattern (Figure 15).The reinforced HEA particles act as a barrier element in the formation of holes and particle dislocation in the corroded surfaces of the P HEA .The corrosion resistance is improved by the presence of HEA elements in higher concentrations.Moreover, the presence of Si in the HEA particles also enhances the corrosion resistance obviously [50].The corrosion morphology of the A HEA and P HEA had instinctual corrosion behaviour due to the presence of HEA particles.However, a pit-free surface is exhibited on the A HEA (Figure 14d).The oxide layers are interconnected that form a network to resist corrosion under the NaCl environment.A more stable and thick oxide layer of corrosion products forms on the A HEA surface that improves corrosion resistance.The electrochemical analysis reveals that the formation of oxide layers on the corroded surfaces hinders the corrosion progress under the 3.5 wt.% NaCl environment.The uniform grain structure of A HEA also reduces the corrosion rate.A better corrosion resistance is appeared on the A HEA and confirms with high peaks of the Cr 2 O 3 and TiO 2 oxides along with the fcc phase structure from the XRD pattern.

Hot Corrosion behaviour
The influence of annealing on the hot corrosion behaviour of processed samples under the salt mixture  A and B are evaluated at a temperature of 800°C.In general, the samples exposed in the salt mixture environment are governed by three stages such as incubation period, initiation step, and propagation period (Figure 16) [53].During the incubation period, the reaction is initiated within a few minutes after the salt mixture film is applied on the surface of the samples and temperature reaches 800°C.The presence of reactive compounds such as sulfur, and oxides in the salt environment starts the interaction with the oxide layer.However, no significant corrosion is observed and the induced reaction between the corrosive species with oxides is similar to normal oxidation.In the initiation stage, a protective layer on the sample starts to deform by the corrosive species.The existence of the incubation period is accelerating the corrosion attack by the elements of the sample at the inner surface.The corrosion pits are formed by increasing corrosive deposits, and attack of grain boundaries under the initiation stage.The localized corrosion such as cracks and pits exhibit on the steel surface.The initiation step is one of the significant stages to explore the corrosion nature.The corrosion damage is progressed with severe corrosion attacks on the sample surface caused by corrosion products such as metal oxide and sulfides during the propagation stage.The induced corrosion pits accelerate the degradation process and the corrosion pits infiltrate the steel base more deeply.The corrosion rate rapidly increases by nitrides and sulfides during the propagation period.The steel surfaces are deformed through the formation of cavities, cracks, and larger pits.The materials are delaminated continuously at the end of the propagation stage [54,55].
The process temperature of hot corrosion is 800°C, which is higher than the eutectic temperature of V 2 O 5 , Na 2 SO 4 , and NaCl.The applied salt film on the surface of the samples is melted under the experimental condition [56].The mass gain kinetics, formation of oxide layers, corrosion products, and corrosion rate are observed on the processed samples under the salt mixtures A and B at 800°C for 50 h.The mass gain of corroded samples is exposed as a parabola curve for the salt mixtures A and B environments at different oxidation times (Figure 17a,b).The profile of kinetic curves indicates that the mass gain is increasing with the increment of exposure time in hot corrosion.A maximum mass gain of 0.0526 mg/cm 2 is measured on the P Base under the salt mixture B which is 17.9% higher than the salt mixture A environment.Moreover, 0.0436 mg/cm 2 , 0.0312 mg/cm 2 , and 0.0236 mg/cm 2 of mass gain are observed on the A Base , P HEA , and A HEA respectively under the salt mixture B and which is 17.2%, 23.%, and 20.4% higher than the salt mixture A environment.The elements S, O, V, and Cl present in the salts penetrate the surface of the P Base through cracks and pores which leads to higher mass gain than the A Base [57].The exposure duration, temperature, and quantity of deposition are the major factors that influence mass gain under hot corrosion [55].The A Base and A HEA are free from cracks, and pores leading to a decrease in the corrosion rate at 800°C.Both processed base samples exhibit more mass gain as compared to the processed HEA samples.It showcases the influence of reinforced HEA particles and the formation of an oxide layer.The barrier effect is induced by the reinforced HEA particles that impede severe corrosion at 800°C.A significant hot corrosion rate is observed under salt mixture B due to the synergistic effect of NaCl, Na 2 SO 4 along with V 2 O 5 .
The SEM images of the P HEA and A HEA under salt mixture A at 800°C to investigate the annealing effect is shown in Figure 18.The pits are generated on the P HEA corroded surface when exposed to salt mixture A environment (Figure 18a).A large spallation area along with etch pits and a dense acicular oxide layer appeared on the P HEA surface.The cracks with irregular corrosion products are observed on the P HEA surface than the A HEA (Figure 18b).The pits are surrounded by acicular oxides, which is a dominant factor for hot corrosion.The oxides of Al 2 O 3 and Fe 2 O 3 are loosely surrounded by corroded surfaces which are confirmed by the XRD pattern (Figure 18c) [58].The cracks are formed by black oxides (Fe 3 O 4 ) which is a more dominant diffraction peak at the surface of P HEA .The surface of the P HEA is diffused through the oxide defects and creates direct contact with base materials.The acid fluxing models are generated by hot corrosion at 800°C [56].The surface of the P HEA is corroded severely along the grain boundaries due to the higher energy, and the equilibrium position of atoms at the grain boundary is varnished.Hence, more defects are formed on the grain boundary.These factors lead to corrosion easily around the area of grain boundary than on the inner side.The crack and peel-off are exhibited on the surface of corroded samples by the loose contact of the oxide layer with salt.Besides, the spallation area exhibits cracks and oxide in the form of clusters.The Cr and Al-oxides have been observed on the A HEA under salt mixture A (Figure 18c).The dark phases appear on some regions of the A HEA indicating corrosion products of chloride and sulfide oxides [59].Moreover, a few regions of the A HEA surface exhibit deep pores.The elements present in the HEA particles form oxides by reacting with O À 2 ions of salt mixture film due to the strong affinity of the elements of HEA with O À 2 ions.Meanwhile, the formed ions are diffused with O À 2 ions in the salt (or) oxide interface to the atmosphere interface.The developed ions are volatilized and released O À 2 to reform oxide [56].The formation of passive films on the surface of the A HEA acts as a barrier for material dissolution [60].The grain refinement by FSP and annealing implies a great potential to improve the corrosion resistance of steel [61].Figure 18d shows the presence of elements on the corroded surface of A HEA under the salt mixture A. The reinforced HEA particles and the elements of the salt mixture are observed in the corroded surface evince the intense corrosion under the salt mixture A. The formation of corrosion products such as Al 2 O 3 , Fe 2 O 3 , Fe 3 O 4 , and TiO 2 under the salt mixture A is verified by the XRD pattern (Figure 18c).
The corrosion morphology of P HEA and A HEA under the salt mixture B environment is shown in Figure 19.Some regions of P HEA exhibit more pores and cracks   attributed to excessive corrosion nature of V 2 O 5 (Figure 19a).The few white phases and more pores on the P HEA indicate dense corrosion than the A HEA after exposing to salt mixture B [62].The pores of corrosion products and unstable layers of oxides are peeling off from the base sample during the progression of the hot corrosion [57].The Cr 2 O 3 and Al 2 O 3 phases are enhanced at the interface of the HEA with the base sample due to the increased oxidation effect in a hot corrosion environment (Figure 19c).An intense oxidation is observed on the corroded samples by the existence of V 2 O 5 in salt mixture B. Subsequently, the unprotective oxides are formed by dissolving protective oxides at the interface of oxide layers and molten salt.The combined effect of NaCl and V 2 O 5 present in salt mixture B produces more oxidation as compared to the salt mixture A environment [63] The deep cracks and intense spallation are observed on the P HEA than the A HEA which demonstrates the severe degradation on the surface.The addition of V 2 O 5 along with NaCl and Na 2 SO 4 attributes a severe spallation under hot corrosion at 800°C [64].The SO 4 2− present in the Na 2 SO 4 salt leads to oxidation as per the acid-alkali melting mechanism.The Cl À ions are reacted with the oxygen under the salt mixture environments at 800°C and more oxides are formed due to increasing O 2À activity [63].
The refined grains are induced on the A HEA by the effect of FSP along with annealing that generates uniform corroded surfaces under the salt mixture B (Figure 19b).The grain refinement and evenly distributed HEA particles attributes the formation of micro cracks, oxides layer and Cl À ions under salt mixture B environment [65].The Cr 2 O 3 oxide layer is increased obviously and Cr-rich layer acts as an excellent barrier agent in the A HEA at high temperature [63].Many research works infer the elemental composition, reinforced HEA particles, and the formation of passive films on the corroded surfaces as the dominant factors for corrosion resistance [66,67].The passivity of steel is improved by the formation of a thicker film with a defect-free oxide layer, which is obtained by grain refinement.It includes improving pitting corrosion resistance and Cr-diffusivity.In addition to grain refinement, the formation of texture, and dislocation density are the major parameters for corrosion behaviour [68].The improved corrosion resistance is obtained through the homogeneous chemical distribution of elements by the heat treatment process.Generally, the high temperature attributes to reduced Gibbs free energy of reinforced HEA elements leading to the phase stability and impediment of intermetallic growth.A high corrosion resistance is obtained on the A HEA than P HEA under the salt mixture B. The combined effect of FSP with annealing processes leads to a more homogeneous microstructure on the A HEA [30].The formation of an oxide layer and the presence of elements in the corroded surfaces is confirmed by elemental mapping through EDS analysis of A HEA (Figure 19d).The elements of Al, Cl, O, and Ti are observed on the corroded surface.The formed oxide and their products under the salt mixture B environment are confirmed by XRD peaks.

Conclusion
The ball-milled lightweight AlSiBeTiV HEA powders are reinforced to SS410 base sample through FSP and subsequently annealing is carried out and properties are evaluated.The synergetic effect of FSP along with annealing improves the microhardness by refined grain structure.The electrochemical and hot corrosion behaviours of processed samples are investigated and the outcomes of the annealed sample are compared with the unannealed sample.The morphological evaluation of the corroded surface of A HEA is conducted and conclusions are drawn as follows, • The AlSiBeTiV HEA powder with irregular fragments and average particle size of 15 µm is exhibited.The contributed principal elements in the HEA are confirmed by EDS analysis.XRD pattern verifies the presence of fcc phase structure on the ball-milled HEA powders.• The SZ of A HEA exhibits 23.3% reduced grains by the effect of annealing at 600°C.The refined grains with an average size of 0.527 µm are evenly distributed along the SZ which are examined by EBSD evaluation.• The refined grains by annealing, DRX, SPD, and Hall-Petch relationship are attributed to the improved microhardness of 672 HV which is 29.7% higher than the P HEA .• The A HEA exhibits a reduced corrosion rate of 47.8% over the P HEA under 3.5 wt.% NaCl environment.The reinforced HEA particles, refined grains by FSP along with annealing, and formation of stable oxide layers improve the corrosion resistance which is confirmed by the Nyquist plot and polarization resistance.• Higher corrosion resistance is exhibited on the A HEA over the P HEA due to the formation of a protective layer against hot corrosion at 800°C.Besides, the mass gain of A HEA is delayed compared to the P HEA by the refined grain structure due to the combined effect of FSP and annealing.The processed samples are severely corroded when it is exposed to salt mixture B than salt mixture A environment due to the presence of V 2 O 5 .
The annealing at 600°C plays a significant role in improving microhardness and corrosion behaviours at both room and high temperature through refined grains.The synergetic effect of FSP and annealing the HEA reinforced samples suits better in corrosion environment applications at ambient and elevated temperatures such as gas turbine blades in aerospace, shipbuilding, offshore marine applications, chemical and nuclear industries.

Figure 1 .
Figure 1.Sequence of present research work.

Figure 5 .Figure 6 .
Figure 5. (a) Line mapping, (b) Elements present across the mapped line of the P HEA .

Figure 7 .
Figure 7. (a) Elemental mapping and its distribution, (b) EDS mapping of A HEA at 600°C.

Figure 13 .
Figure 13.Corrosion rate of processed samples.

Figure 15 .
Figure 15.XRD patterns of P HEA and A HEA .

Figure 17 .
Figure 17.Corrosion kinetic curves of samples (a) Salt mixture A, (b) Salt mixture B at 800°C.

Figure 18 .
Figure 18.(a) SEM image of P HEA , (b) SEM image of A HEA , (c) XRD patterns of P HEA and A HEA , (d) Elemental mapping of A HEA under salt mixture a environment.

Figure 19 .
Figure 19.(a) SEM image of P HEA , (b) SEM image of A HEA , (c) XRD patterns of P HEA and A HEA , (d) Elemental mapping of A HEA under salt mixture B environment.

Table 1 .
Elements of HEA powder.
Figure 2. Macroscopic image of the processed sample.

Table 3 .
Corrosion parameters of PDP.